Effect of inlet boundary-layer thickness and structure on heat transfer in a supersonic nozzle.
BACK, L. H., CUFFEL, R. F. /CALIFORNIA INST. OF TECH., JET PROPULSIONLAB., HEAT TRANSFER AND FLUID DYNAMICS GROUP, MASSIER, P. F.
JOURNAL OF SPACECRAFT AND ROCKETS ; 5 , 1 ; 121-123
1968
Article (Journal)
Electronic Resource
English
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